Airbus Helicopters H125 vs Airbus Helicopters H130 vs Airbus Helicopters H175 vs Leonardo Aw139
The Airbus Helicopters H125 and H130 are both light single‑engine helicopters aimed at utility and passenger transport, while the H175 and Leonardo AW139 are medium twin‑engine aircraft suited to offshore, SAR, and corporate/VIP missions. In passenger capacity, the H125 typically carries a pilot plus up to about five passengers, whereas the more cabin‑focused H130 usually accommodates a pilot plus up to six or seven passengers depending on configuration. Moving up in class, both the H175 and AW139 generally seat around a dozen people in high‑density layouts; in typical offshore or corporate layouts they commonly carry about eight to twelve passengers plus crew. On range, the light singles (H125/H130) are usually used for shorter legs, with typical operational ranges in the few‑hundred‑nautical‑mile class depending heavily on fuel, payload, and reserves. The medium twins (H175/AW139) generally offer longer legs and higher cruise speeds, with ranges typically around the 400–500+ nautical mile class, again varying by tanking and mission equipment. Overall, H125 prioritizes versatility and hot‑and‑high performance, H130 emphasizes quiet, roomy passenger comfort, and H175/AW139 deliver higher payload and longer‑range capability.
| Spec | AIRBUS H125 | AIRBUS H130 | AIRBUS H175 | AGUSTA / LEONARDO AW139 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 13.53 | $ 11.69 |
| Min Crew | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 7 | 18 | 17 |
| Flight Rules | VFR | VFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Leonardo |
| Aircraft Name | H125 | H130 | H175 | AW139 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 573 | 573 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.75 | $ 0.69 |
| Max Cabin Seats | 5 | 5 | 18 | 15 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 6797 | 4701 |
| Standard Cabin Seats | 4 | 4 | 16 | 15 |
| Direct Operating Cost | $ 627 | $ 640 | $ 2,016 | $ 1,929 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 128 | 149 | 165 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $17,900,000 | $15,900,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 7 | 18 | 17 |
| Max Cabin Seats | 5 | 5 | 18 | 15 |
| Standard Cabin Seats | 4 | 4 | 16 | 15 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arriel 2D | PT6A-67E | PT6C-67C |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 3500 | 5000 |
| Horsepower | 847 | 952 | 1775 | 1679 |
| No. of Engines | 1 | 1 | 2 | 2 |
| Fuel Capacity (gal) | 143 | 143 | — | 414 |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.5 | 59.2 | 54.7 |
| Overall Height (ft) | 10 | 11.1 | 17.5 | 16.4 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 48.5 | 54.7 |
| Cabin Volume (cu. ft) | — | — | 423.8 | 282 |
| Baggage Volume Ext. (cu. ft) | — | — | 81.9 | 120 |